Fully 3D ship hydroelasticity: monolithic versus partitioned strategies for tight coupling

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<big>'''Fully 3D ship hydroelasticity: monolithic versus partitioned strategies for tight coupling'''</big></div>

Borja Servan-Camas<sup>1,*</sup>, Daniel Di-Capua, D.<sup>1,2</sup>, Julio Garcia-Espinosa<sup>1,2</sup>, and Daniel Sa-Lopez<sup>3</sup>.

<sup>1</sup> Centre Internacional de Mètodes Numèrics a l’Enginyeria (CIMNE), Edifici C1, Campus Norte, UPC, Gran Capitán s/n, 08034 Barcelona, Spain

<sup>2</sup> Universidad Politécnica de Cataluña (UPC), C. Gran Capitan s/n, Campus Nord, 08034 Barcelona, Spain

<sup>3</sup> Compass Ingeniería y SItemas, C. Gran Capitan s/n, Campus Nord, 08034 Barcelona, Spain

<sup>(*)</sup> Corresponding author
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==Abstract==

This paper analyzes the partitioned and monolithic strategies to simulate tightly coupled hidroelastic problems. The seakeeping hydrodynamics solver used is based on a first-order linear time-domain FEM model with forward speed and double-body linearization. The structural dynamics solver is based on a full 3D time-domain FEM with corotational shell elements accounting for the geometric non-linearity. Both solvers are implemented under the same programming framework, which allows to implement the monolithic strategy, and to minimize the communication overheads of the partitioned strategy. Two case studies are used to test and compare the partitioned and monolithic coupling: a flexible catamaran in oblique waves, and a large floating reticulated structure made of fiber reinforced plastic. In both cases, the monolithic strategy is between three and four times faster than the partitioned strategy.

This project has been developed under the H2020 project FIBRESHIP aimed at developing the technology to design and build the structure of large-length vessels in fiber reinforced polymers.

==1. Introduction==

Current rules and regulations cover adequately most of the aspects relevant to the structural ship design. However, several essential aspects are vaguely addressed, or rely upon a case-by-case approval process by the authorities. Among these aspects we can highlight different phenomena involving the hydroelastic response, such as springing, whipping and racking, resulting in dynamically induced hull stresses.

<span id='_Ref41721997'></span>The above mentioned dynamic phenomena can increase significantly the hull stresses. Therefore, in some critical cases, the quasi-static approach to hydroelasticity used by the current rules and regulations can largely underestimate the actual design loads. Hence, in some cases, it is required to study the coupled hydroelastic response of the structure [<span id='cite-1'></span>[[#1|1]]] by carrying out experimental tests at model scale and/or running computer analysis.

<span id='_Ref36879644'></span><span id='_Ref36880186'></span><span id='_Ref36280404'></span><span id='_Ref36310740'></span><span id='_Ref36315829'></span><span id='_Ref36315668'></span><span id='_Ref36310896'></span>There are two different methods for hydroelastic model testing. The first one and least popular, due to its complexity and cost [<span id='cite-2'></span>[[#2|2]]], is to build a model using some elastic material trying to scale down the elastic behavior of the ship [<span id='cite-3'></span>[[#3|3]],<span id='cite-4'></span>[[#4|4]]]. In this method, the evaluation of the vibration modes cannot be estimated properly in fully elastic models due to larger internal damping [<span id='cite-5'></span>[[#5|5]]]. The second one (and the most popular) is to build a segmented model connected by a flexible beam with similar global elastic properties [<span id='cite-_Ref36879644'></span>[[#_Ref36879644|2]],<span id='cite-6'></span>[[#6|6]],<span id='cite-7'></span>[[#7|7]],<span id='cite-8'></span>[[#8|8]],<span id='cite-9'></span>[[#9|9]],<span id='cite-10'></span>[[#10|10]],<span id='cite-11'></span>[[#11|11]]]. The number of segments depend on the number of displacement modes to model. The pros and cons of both methodologies were analyzed and compared in [<span id='cite-_Ref36880186'></span>[[#_Ref36880186|5]]], where the advantages of the second option are highlighted.

Anyhow, a major drawback of both testing techniques is than only global hydroelastic effects can be modelled and measured. The only alternative to analyze more local effects is the use of numerical simulations.

<span id='_Ref36314775'></span><span id='_Ref36316963'></span><span id='_Ref36315610'></span><span id='_Ref36317947'></span><span id='_Ref36311150'></span><span id='_Ref36365834'></span><span id='_Ref36317765'></span>The numerical simulation of hydroelasticity involve the coupling between the hydrodynamics and the structural dynamics. The most common approach is to solve the hydrodynamics with 3D potential flow using the boundary element method (BEM), and the structural dynamics with the 1D beam model using the finite element method (FEM) [<span id='cite-_Ref36315668'></span>[[#_Ref36315668|10]],<span id='cite-_Ref36310896'></span>[[#_Ref36310896|11]],<span id='cite-12'></span>[[#12|12]],<span id='cite-13'></span>[[#13|13]],<span id='cite-14'></span>[[#14|14]],<span id='cite-_Ref36311150'></span>[[#_Ref36311150|18]]]. Several works have extended the fluid dynamics model, by solving the Navier Stokes equations instead of the potential flow equations [<span id='cite-15'></span>[[#15|15]],<span id='cite-16'></span>[[#16|16]],<span id='cite-17'></span>[[#17|17]]]. From the structural point of view, just a few authors have used more sophisticated approaches such as the 1D-3D FEM hybrid method [<span id='cite-_Ref36316963'></span>[[#_Ref36316963|12]],<span id='cite-18'></span>[[#18|18]]] or directly coupling a fully 3D FEM [<span id='cite-19'></span>[[#19|19]]]. Most of the works only consider the linear response, while the most common approach for modeling the structure is based on the superposition of modes [<span id='cite-_Ref41721997'></span>[[#_Ref41721997|1]],<span id='cite-_Ref36315829'></span>[[#_Ref36315829|9]],<span id='cite-_Ref36317947'></span>[[#_Ref36317947|16]],<span id='cite-_Ref36317765'></span>[[#_Ref36317765|19]]], regardless the dimension of the model (1D beam or 3D).

<span id='_Ref40861036'></span>In order to be able to simulate transient or non-linear responses, it is necessary to work in the time-domain [<span id='cite-_Ref41721997'></span>[[#_Ref41721997|1]]]. In the context of potential flow solvers, Cummins [<span id='cite-20'></span>[[#20|20]]] proposed the use of the impulse response function to transfer the results from the frequency-domain to the time-domain, and different authors have followed this approach [<span id='cite-_Ref36315829'></span>[[#_Ref36315829|9]], <span id='cite-_Ref36315668'></span>[[#_Ref36315668|10]], <span id='cite-_Ref36310896'></span>[[#_Ref36310896|11]], <span id='cite-_Ref36365834'></span>[[#_Ref36365834|18]]]. It requires to perform the structural modal analysis, and to solve the wave radiation problem for the corresponding displacement modes. A main drawback of this approximation is that it cannot accurately capture the local stresses -essential to predict failure- which mainly depend on local strains [<span id='cite-21'></span>[[#21|21]]]. In order to overcome this drawback, it is necessary to solve in the time-domain the full 3D coupled hydroelastic problem.

<span id='_Ref36836714'></span>Solving the full hydroelasticity problem in the time-domain is much less common in the literature due to its complexity and computational cost. In [<span id='cite-22'></span>[[#22|22]]] a partitioned strategy was implemented to analyze the interaction between the free surface and the seals of a surface effect ship. The hydrodynamic model was based on potential flow with forward speed, and the results were compared with experimental tests. A recent work [<span id='cite-_Ref36315610'></span>[[#_Ref36315610|14]]] solved the global hydroelastic response of a S175 ship using a coupled BEM–FEM approach and compared the results against the equivalent rigid body problem.

Very flexible floating structures with natural frequencies close to the wave frequency range are rare yet. An example could be two rigid bodies connected by some flexible structure (as the first case study that will be presented in this work). A reason might be the lack of tools to assess their design with affordable computational times.

<span id='_Ref36836716'></span><span id='_Ref36836720'></span><span id='_Ref71620710'></span><span id='_Ref55627692'></span>In this work, a full time-domain hydroelastic model using a FEM-FEM coupled approach is presented. On the one hand, the hydrodynamics model is based on a first-order linear potential flow and takes into account the forward speed effect using the double body linearization. The velocity potential is solved using the FEM along with the SUPG for the free surface boundary condition [<span id='cite-23'></span>[[#23|23]],<span id='cite-24'></span>[[#24|24]],<span id='cite-25'></span>[[#25|25]]]. On the other hand, the structural dynamics is solved using a co-rotational shell FEM model that takes into account the geometric non-linearity.

From the numerical point of view, two strategies can be adopted in this work to solve strongly coupled hydroelastic problems in the time domain. The first one is the partitioned coupling, where to different solvers are tightly coupled via the exchange of coupling variables in an iterative process. The second one is the monolithic coupling, where both models are implemented in a single code, allowing to formulate and solve the equations governing the flow and the structure dynamics with a single solver.

The partitioned coupling, also referred as iterative coupling, is the most common approach for coupled problems because it leverages existing investment in legacy codes development and permits those codes to continue to evolve independently [<span id='cite-_Ref40861036'></span>[[#_Ref40861036|21]]]. This approach allows choosing the most effective solution for each solver, and makes easier the code development. However it requires a robust coupling algorithm that respect conservation laws, and an iterative algorithm that ensure convergence (which is not trivial). This coupling can be computationally expensive due to the iteration process required within each time step and the communication overheads.

Monolithic coupling has the advantage that the coupling occurs at the governing system level, avoiding an iterative process between solvers, which is the tightest scheme available. Since there is a single data structure that embodies discretization of the coupled system of fluid and structure, there is no communication overheads. However, the coupled system contains very different types of field variables, leading to a numerically ill-conditioned system of equations [<span id='cite-_Ref40861036'></span>[[#_Ref40861036|21]]].

Both coupling strategies have been implemented and the objective of this work is to compare them in terms of robustness and computational efficiency.  The paper is organized as follows. In Section 2, we present the statement of the seakeeping model. It is based on a time-domain wave diffraction-radiation solver based on the finite element method (FEM). In Section 3, we present the structural model, which is based on geometrical non-linear shell finite elements. In section 4, the two coupling strategies implemented are presented. In section 5 two application examples are shown: the first one is a flexible catamaran in oblique waves; and the second one is the analysis of large floating structure. Finally in Section 5, we discuss the different results and arrive at some conclusions.

==2. Seakeeping model==

The seakeeping model used in this work is a first-order linear time-domain wave diffraction-radiation solver based on the finite element method (FEM). Non-linearities, such as wet surface intermittency, quadratic velocity term in pressure equation, non-linear wave effects, or drag forces, are not considered.  The seakeeping model was developed in-house and integrated in the commercial package SeaFEM [<span id='cite-26'></span>[[#26|26]]]. The governing equations, respect to a global frame of reference located at the mean water level with OXY representing the horizontal plane, and OZ the upward vertical direction, are given by:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\Delta \varphi =0</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">in\, \Omega</math> ,
|}
|  style="text-align: right;white-space: nowrap;"|(1)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\partial }_{t}\xi +(\mathit{\boldsymbol{U+}}{\nabla }_{h}\varphi )\mathit{\boldsymbol{\cdot }}{\nabla }_{h}\xi -</math><math>{\partial }_{z}\varphi =0</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, z=0</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(2)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\partial }_{t}\varphi +\mathit{\boldsymbol{U\cdot }}{\nabla }_{h}\varphi +</math><math>\frac{1}{2}{\nabla }_{h}\varphi \mathit{\boldsymbol{\cdot }}{\nabla }_{h}\varphi +</math><math>g\xi ={P}_{fs}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, z=0</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(3)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\mathit{\boldsymbol{v}}}_{\varphi }\cdot {\mathit{\boldsymbol{n}}}_{p}\, =-{\mathit{\boldsymbol{v}}}_{p}\cdot {\mathit{\boldsymbol{n}}}_{p}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, P\in {\Gamma }_{B}</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(4)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\mathit{\boldsymbol{v}}}_{\varphi }\cdot {\mathit{\boldsymbol{n}}}_{p}=0</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, P\in {\Gamma }_{S}</math>,
|}
|  style="text-align: right;white-space: nowrap;"|
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{P}_{p}=-\rho g({z}_{p}+{r}_{pz})-\rho \left( \frac{\partial \varphi \, }{\partial t}+\right. </math><math>\left. \mathit{\boldsymbol{U\cdot }}\nabla \varphi +\frac{1}{2}\nabla \varphi \mathit{\boldsymbol{\cdot }}\nabla \varphi \right) ,</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| 
|}
|  style="text-align: right;white-space: nowrap;"|<span id='_Ref35455561'></span>(5)
|}


Where <math display="inline">\, \varphi</math>  is the velocity potential ( <math display="inline">{\mathit{\boldsymbol{v}}}_{\varphi }=</math><math>\nabla \varphi</math> ), <math display="inline">\xi</math>  is the free surface elevation, <math display="inline">\Omega</math>  is the fluid domain, <math display="inline">{P}_{fs}</math> is the free surface pressure, <math display="inline">z=</math><math>0</math> represents the still water level, <math display="inline">\, {\nabla }_{h}=</math><math>(\partial /\partial x,\partial /\partial y)</math> is the horizontal gradient operator,  <math display="inline">{\Gamma }_{B}</math> is the wetted Surface of a floating body, <math display="inline">{\Gamma }_{S}</math> is the sea bottom Surface, <math display="inline">{n}_{p}</math> is a normal vector to a Surface at point P, <math display="inline">{v}_{p}</math> is the velocity of point p, <math display="inline">{z}_{p}</math> is the initial vertical position of point P, and <math display="inline">{r}_{pz}</math> is the vertical displacement of P.

The solution can be split into the incident and diffracted-radiated wave components:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\varphi =\psi +\phi</math> 
|}
| 
{| style="margin:auto;width: 100%;"
|-
| 
|}
|  style="text-align: right;text-align: right;white-space: nowrap;"|(6)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\xi =\zeta +\eta</math> 
|}
| 
{| style="margin:auto;width: 100%;"
|-
| 
|}
|  style="text-align: right;text-align: right;white-space: nowrap;"|(7)
|}


where <math display="inline">\psi</math>  and <math display="inline">\zeta</math>  are the velocity potential and wave elevation respectively for the incident wave field, and <math display="inline">\phi</math>  and <math display="inline">\eta</math>  are the velocity potential and free surface elevation respectively for the diffracted-radiated waves respectively. The incident wave field is described by the Airy wave analytical solution. Introducing the separation of variables into the governing equations, the wave diffraction-radiation problem is obtained in terms of <math display="inline">\phi</math>  and <math display="inline">\eta</math>  as independent variables.

The free surface pressure is <math display="inline">{P}_{fs}=0</math>  in a region close to the body (near field), but beyond the near field, <math display="inline">{P}_{fs}=</math><math>\kappa \left( \mathit{\boldsymbol{x}}\right) {\phi }_{z}</math>, where <math display="inline">\kappa \left( \mathit{\boldsymbol{x}}\right)</math>  is a factor that grows with the distance to the body. This term is used to dissipate the diffracted-radiated waves [<span id='cite-_Ref36836716'></span>[[#_Ref36836716|23]], <span id='cite-_Ref55627692'></span>[[#_Ref55627692|25]]]. Moreover. Details on the wave diffraction-radiation governing equations can be found in [<span id='cite-_Ref36836714'></span>[[#_Ref36836714|22]], <span id='cite-_Ref36836716'></span>[[#_Ref36836716|23]], <span id='cite-_Ref36836720'></span>[[#_Ref36836720|24]]].

In this work the numerical solution using FEM of the above system reported in [<span id='cite-_Ref36836714'></span>[[#_Ref36836714|22]], <span id='cite-_Ref36836716'></span>[[#_Ref36836716|23]], <span id='cite-_Ref36836720'></span>[[#_Ref36836720|24]]] will be used. It requires to solve the following system of equations:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\boldsymbol{L}}}\boldsymbol{\phi }={\boldsymbol{b}}^{B}+{\boldsymbol{b}}^{{Z}_{0}}+</math><math>{\boldsymbol{b}}^{S},</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(8)
|}


Where <math display="inline">\overline{\overline{\boldsymbol{L}}}</math> is the Laplacian Matrix, and the right hand side is obtained summing up the vectors <math display="inline">{\boldsymbol{b}}^{B}</math>, <math display="inline">{\boldsymbol{b}}^{{Z}_{0}}</math>, and <math display="inline">{\boldsymbol{b}}^{S}</math>. The right hand side are obtained from discretizing the boundary conditions using FEM as in [<span id='cite-_Ref36836716'></span>[[#_Ref36836716|23]],<span id='cite-_Ref71620710'></span>[[#_Ref71620710|24]],<span id='cite-_Ref55627692'></span>[[#_Ref55627692|25]]]. The above system can be written clustering the nodes lying on the body surface as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\left[ \begin{matrix}{\overline{\overline{\boldsymbol{L}}}}_{II}&{\overline{\overline{\boldsymbol{L}}}}_{I{\Gamma }_{B}}\\{\overline{\overline{\boldsymbol{L}}}}_{{\Gamma }_{B}I}&{\overline{\overline{\boldsymbol{L}}}}_{{\Gamma }_{B}{\Gamma }_{B}}\end{matrix}\right] {\left[ \begin{matrix}{\boldsymbol{\phi }}_{I}\\{\boldsymbol{\phi }}_{{\Gamma }_{B}}\end{matrix}\right] }^{n+1}=</math><math>{\left[ \begin{matrix}{\boldsymbol{b}}_{I}\\{\boldsymbol{b}}_{{\Gamma }_{B}}\end{matrix}\right] }^{n+1}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(9)
|}


where <math display="inline">{\boldsymbol{b}}_{{\boldsymbol{\Gamma }}_{\mathit{\boldsymbol{B}}}}</math> contains the velocities of a point lying on the structure boundary. In the case of having  forward speed, the free surface boundary condition is integrated using the FEM SUPG scheme with the double body lineariazation, and the numerical details can be found in [<span id='cite-_Ref36836714'></span>[[#_Ref36836714|22]], <span id='cite-_Ref36836716'></span>[[#_Ref36836716|23]]]. For the zero forward speed, a fourth order compact Padé scheme is used for the free surface, and the numerical details can be found in [<span id='cite-_Ref36836714'></span>[[#_Ref36836714|22]], <span id='cite-_Ref36836720'></span>[[#_Ref36836720|24]]].

==3. Structural model==

<span id='_Ref71620876'></span><span id='_Ref40985077'></span><span id='_Ref71620881'></span>The structural dynamic model used in this work is based on geometrical non-linear shell finite elements. The geometrical non-linear model is based on the corotational method developed by Felippa and Haguen in [<span id='cite-27'></span>[[#27|27]]]. The core element used by the corotational shell model is a 3-node element with three translations and three rotations per node, which is obtained by the combination of a membrane element and a plate element. The membrane element is based in the optimal triangle element with drilling rotation developed by Felippa in [<span id='cite-28'></span>[[#28|28]]], while the plate element is based in the classical DKT element first introduced in [<span id='cite-29'></span>[[#29|29]]]. This element has shown better performance that the standard bilinear quadrilateral element generally used in marine applications [<span id='cite-_Ref40985077'></span>[[#_Ref40985077|28]]].

The algorithm used for the time-integration is based in the approximately energy conserving scheme presented by Almeida and Awruch in [<span id='cite-30'></span>[[#30|30]]]. The complete model has been developed in-house and integrated within the commercial package RamSeries [<span id='cite-31'></span>[[#31|31]]]. The governing equations of the model are given by:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\mathit{\boldsymbol{div}}\left( \mathit{\boldsymbol{\sigma }}\right) +\mathit{\boldsymbol{b}}=</math><math>\mathit{\boldsymbol{\rho }}\ddot{\mathit{\boldsymbol{u}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">in\, {\Omega }_{s}</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(10)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\mathit{\boldsymbol{u}}=\overline{\mathit{\boldsymbol{u}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, P\in {S}_{u}</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(11)
|-
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\mathit{\boldsymbol{\sigma }}\cdot \mathit{\boldsymbol{n}}=\overline{\mathit{\boldsymbol{t}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math display="inline">on\, P\in {S}_{\sigma }</math>,
|}
|  style="text-align: right;white-space: nowrap;"|(12)
|}


where <math display="inline">\mathit{\boldsymbol{\sigma }}</math> is the stress tensor, <math display="inline">\mathit{\boldsymbol{b}}</math> is the mass force vector, <math display="inline">{\Omega }_{s}</math> is the structural domain, <math display="inline">\mathit{\boldsymbol{u}}</math> is the structural displacement vector field, <math display="inline">{S}_{u}</math> is the part of the structural external surface with prescribed displacements <math display="inline">\overline{\mathit{\boldsymbol{u}}}</math>, <math display="inline">{S}_{\sigma }</math> is the part of the structural external surface with prescribed tractions <math display="inline">\overline{\mathit{\boldsymbol{t}}}.</math> The numerical solution of the above system requires the numerical solution of the following system of equations:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\boldsymbol{S}}}{\Delta \boldsymbol{u}}^{n+1}={\boldsymbol{a}}^{n+1}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(13)
|}


where <math display="inline">n+1</math> is the current time step,  <math display="inline">\overline{\overline{\boldsymbol{S}}}</math> is the tangent stiffness Matrix, <math display="inline">\Delta {\boldsymbol{u}}_{I}</math> is the incremental displacement vector of the nodes located in the interior, <math display="inline">{\Delta \boldsymbol{u}}_{{\Gamma }_{B}}</math> is the incremental displacement of the nodes in contact with the fluid, and <math display="inline">\boldsymbol{a}</math> is the right hand side which is obtained from the discretization of the boundary conditions using FEM [<span id='cite-_Ref71620876'></span>[[#_Ref71620876|27]],<span id='cite-_Ref40985077'></span>[[#_Ref40985077|28]],<span id='cite-_Ref71620881'></span>[[#_Ref71620881|29]]]. The system above can be written clustering the nodes lying on the body surface as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\left[ \begin{matrix}{\overline{\overline{\boldsymbol{S}}}}_{II}&{\overline{\overline{\boldsymbol{S}}}}_{I{\Gamma }_{B}}\\{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}I}&{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}{\Gamma }_{B}}\end{matrix}\right] {\left[ \begin{matrix}\Delta {\boldsymbol{u}}_{I}\\{\Delta \boldsymbol{u}}_{{\Gamma }_{B}}\end{matrix}\right] }^{n+1}=</math><math>{\left[ \begin{matrix}{\boldsymbol{a}}_{I}\\{\boldsymbol{a}}_{{\Gamma }_{B}}\end{matrix}\right] }^{n+1}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|<span id='_Ref36804909'></span>(14)
|}


Where <math display="inline">{\boldsymbol{a}}_{{\boldsymbol{\Gamma }}_{\mathit{\boldsymbol{B}}}}</math> contains the fluid pressure acting on the boundary condition.

==4. Coupling strategies==

The purpose of this section is to present the two coupling strategies implemented to tightly couple the seakeeping hydrodynamics solver and the structural dynamics solver. The coupled problem is sketched in <span id='cite-_Ref488050570'></span>[[#_Ref488050570|Figure 1]].

As presented above, the seakeeping and structural problems will be discretized using the FEM. However, it is not required to use identical discretization for the common boundary  <math display="inline">{\Gamma }_{B}</math> where the interaction occurs will be discretized. Spatial linear interpolators have been used in this work to transfer the fluid pressure to the structure boundary and to transfer the structural displacements to the fluid boundary.

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\left[ {\boldsymbol{P}}_{S,{\Gamma }_{B}}\right] ={\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}\, \left[ {\boldsymbol{P}}_{F,{\Gamma }_{B}}\right]</math> 
|}
|  style="text-align: right;width: 5px;text-align: right;white-space: nowrap;"|(15)
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\left[ {\Delta \boldsymbol{u}}_{F,{\Gamma }_{B}}\right] ={\overline{\overline{\mathit{\boldsymbol{I}}}}}^{S\rightarrow F}\, \left[ {\Delta \boldsymbol{u}}_{S,{\Gamma }_{B}}\right]</math> 
|}
|  style="text-align: right;width: 5px;text-align: right;white-space: nowrap;"|(16)
|}


Where <math display="inline">{\boldsymbol{P}}_{S,{\Gamma }_{B}}</math>''' ''' <math display="inline">{\mathit{\boldsymbol{\Delta }}\boldsymbol{u}}_{S,{\Gamma }_{B}}</math>''', ''' <math display="inline">{\boldsymbol{P}}_{F,{\Gamma }_{B}}</math>''', '''and''' ''' <math display="inline">{\mathit{\boldsymbol{\Delta }}\boldsymbol{u}}_{F,{\Gamma }_{B}}</math>are the fluid pressure and structural displacements at the structural and fluid discretization over <math display="inline">{\Gamma }_{B}</math> respectively, and <math display="inline">{\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}</math> and <math display="inline">{\overline{\overline{\mathit{\boldsymbol{I}}}}}^{S\rightarrow F}</math>''' '''are the corresponding interpolation matrices.

{| style="width: 100%;border-collapse: collapse;" 
|-
|  style="text-align: center;vertical-align: top;width: 100%;"|[[Image:Draft_Garcia-Espinosa_378827043-image1.jpg|390px]] 
|-
|  style="vertical-align: top;"|<span id='_Ref488050570'></span>Figure 1: Fluid-Structure interaction concept.
|}


===4.1 Partitioned coupling===

As introduced above, in the partitioned coupling the different solvers are tightly coupled via the exchange of coupling variables in an iterative process. It has the advantage of solving the seakeeping and structural dynamics independently using the most efficient algorithms for each one. For instance, a deflated preconditioned iterative solver could be used for the seakeeping problem [<span id='cite-_Ref36836720'></span>[[#_Ref36836720|24]]], while a direct solver could be used for the structural solver. The main drawbacks of the partitioned strategy are that it requires a robust iterative algorithm to guarantee the convergence of the solver within every time step and that the exchange of information between the two solvers might introduce large computational overheads.

The seakeeping and structural solvers used in this work have been developed under the same programming framework. The utilities of the OpenMP library [<span id='cite-32'></span>[[#32|32]]] have been used to create two parallel threads to run each solver in parallel and exchange field variables between them at code level. This way, the communication overheads are minimized when compared with coupling two independent solvers.

<span id='cite-_Ref36971180'></span>[[#_Ref36971180|Figure 2]] shows the iterative process implemented for the partitioned coupling. This process consist of 9 steps for every iteration. At first, it was observed that the direct exchange of fluid pressure and structural displacements had convergence issues. Hence, step 6 was introduced, using a constant relaxation factor for the pressure. While convergence can be achieved, it depends on the relaxation factor, which is not so obvious to estimate. Finally the Aitken´s method [<span id='cite-_Ref36836714'></span>[[#_Ref36836714|22]],<span id='cite-33'></span>[[#33|33]]] was implemented and greatly improved the stability, and accelerated the convergence.

{| style="width: 100%;border-collapse: collapse;" 
|-
|  style="text-align: center;vertical-align: top;width: 100%;"|[[Image:Draft_Garcia-Espinosa_378827043-image2.jpg|534px]] 
|-
|  style="vertical-align: top;"|<span id='_Ref36971180'></span>Figure 2: Iterative scheme of partitioned coupling.
|}


===4.2 Monolithic coupling===

In the monolithic coupling, the fluid and structural governing equations are coupled through the common boundary condition. This leads to a coupled system of equations that contains the governing system of equations for the fluid and the structure, and a number of coupling equations that connect the independent variables through the shared boundary condition. As a result, the overall number of degrees of freedom is increased to take into account the effect of the fluid pressure on the structure, and the structural displacements on the fluid.

The procedure developed in this work to obtain the monolithic system of equations is presented below.

The fluid pressure can be decomposed as <math display="inline">P={P}^{H}+{P}^{\psi }+</math><math>{P}^{\phi }</math>, where <math display="inline">{P}^{H}=-\rho g\left( {z}_{p}+{r}_{pz}\right)</math>  is the hydrostatic pressure, <math display="inline">{P}^{\psi }=</math><math>-\rho \frac{\partial \psi \, }{\partial t}</math> is the dynamic pressure induced by the incident wave field, and <math display="inline">{P}^{\phi }=</math><math>-\rho \left( \frac{\partial \phi \, }{\partial t}+\mathit{\boldsymbol{U}}\cdot {\mathit{\boldsymbol{v}}}_{\phi }+\right. </math><math>\left. \frac{1}{2}{\mathit{\boldsymbol{v}}}_{\phi }\cdot {\mathit{\boldsymbol{v}}}_{\phi }\right)</math>  is the dynamic pressure induced by the diffracted and radiated waves. The only pressure component depending on the diffracted- radiated fluid velocity potential is <math display="inline">{P}^{\phi }</math> and, therefore, is the responsible of the coupling. Hence, we can split the residual <math display="inline">{\boldsymbol{a}}_{{\Gamma }_{B}}</math> as   <math display="inline">{\boldsymbol{a}}_{{\Gamma }_{B}}=</math><math>{\boldsymbol{a}}_{{\Gamma }_{B}}^{\ast }+{\boldsymbol{a}}_{{\Gamma }_{B}}^{\phi }({P}^{\phi })</math> and rewrite the equation <span id='cite-_Ref36804909'></span>[[#_Ref36804909|(14)]] as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>\left[ \begin{matrix}{\overline{\overline{\boldsymbol{S}}}}_{II}&{\overline{\overline{\boldsymbol{S}}}}_{I{\Gamma }_{B}}\\{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}I}&{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}{\Gamma }_{B}}\end{matrix}\right] {\left[ \begin{matrix}\Delta {\boldsymbol{u}}_{I}\\{\Delta \boldsymbol{u}}_{{\Gamma }_{B}}\end{matrix}\right] }^{n+1}=</math><math>{\left[ \begin{matrix}{\boldsymbol{a}}_{I}\\{\boldsymbol{a}}_{{\Gamma }_{B}}^{\ast }\end{matrix}\right] }^{n+1}+</math><math>\left[ \begin{matrix}\mathit{\boldsymbol{0}}\\\overline{\overline{\mathit{\boldsymbol{C}}}}\end{matrix}\right] {\left[ \begin{matrix}\mathit{\boldsymbol{0}}\\{\boldsymbol{P}}_{{S,\Gamma }_{B}}^{\phi }\end{matrix}\right] }^{n+1}</math>
|}
|  style="text-align: right;width: 5px;text-align: right;white-space: nowrap;"|(17)
|}


where n is the time step and i is the iteration step,  <math display="inline">{\boldsymbol{a}}_{{\Gamma }_{B}}^{\ast }</math> contains the contribution of the hydrostatic and incident wave pressures. The subscript <math display="inline">S</math> in <math display="inline">{\boldsymbol{P}}_{{S,\Gamma }_{B}}^{\phi }</math> indicates that the corresponding variable is evaluated with the variables in the structure side of the coupling boundary <math display="inline">{\Gamma }_{B}</math>. Similarly, throughout this section, the subscripts <math display="inline">S</math> and <math display="inline">F</math> are used to indicate whether the corresponding variable is evaluated with the variables in the structure or fluid side of the coupling, respectively.

The diffraction-radiation component, <math display="inline">{\boldsymbol{a}}_{{\Gamma }_{B}}^{\phi }</math>, of the residual <math display="inline">{\boldsymbol{a}}_{{\Gamma }_{B}}</math> can be obtained as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{a}}_{{\Gamma }_{B}}^{\phi }\right] }^{n+1}=</math><math>\overline{\overline{\mathit{\boldsymbol{C}}}}{\left[ {\boldsymbol{P}}_{{S,\Gamma }_{B}}^{\phi }\right] }^{n+1}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(18)
|}


The fluid pressure is obtained numerically from the velocity potential using Eq. <span id='cite-_Ref35455561'></span>[[#_Ref35455561|(5)]], as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{P}}_{{F,\Gamma }_{B}}^{\phi }\right] }^{n+1,i+1}\mathit{\boldsymbol{=-}}\rho \frac{1.5{\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n+1,i+1}-2.0{\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n}+0.5{\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n-1}}{\Delta t}\, -</math><math>\rho {\left[ \mathit{\boldsymbol{U\cdot }}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}+\frac{1}{2}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}\mathit{\boldsymbol{\cdot }}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}\right] }^{n+1,i}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(19)
|}


Using the interpolation matrix we obtain:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{P}}_{{S,\Gamma }_{B}}^{\phi }\right] }^{n+1}=\alpha {\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}\, {\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n+1}+</math><math>{\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}\, {\left[ \boldsymbol{d}\right] }^{n+1}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(20)
|}


Where <math display="inline">\alpha =-1.5\rho /\Delta t</math> and:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ \boldsymbol{d}\right] }^{n+1}=-\rho \left( -2.0{\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n}+\right. </math><math>\left. 0.5{\left[ {\boldsymbol{\phi }}_{{\Gamma }_{B}}\right] }^{n-1}\right) /\Delta t-</math><math>\rho {\left[ \mathit{\boldsymbol{U\cdot }}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}+\frac{1}{2}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}\mathit{\boldsymbol{\cdot }}{\boldsymbol{v}}_{\phi }^{{\Gamma }_{B}}\right] }^{n+1,i}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(21)
|}


Furthermore, the fluid body boundary condition term <math display="inline">{\boldsymbol{b}}_{{\boldsymbol{\Gamma }}_{\mathit{\boldsymbol{B}}}}</math>''' '''in eq. (9) comes from imposing that the fluid cannot penetrate the structure. That is to say, the displacement of a point lying on <math display="inline">{\boldsymbol{\Gamma }}_{\mathit{\boldsymbol{B}}}</math>''' '''along the normal direction''' '''must''' '''match the one of the fluid particle at the same location. Hence, we can establish a relationship between the structural displacement and the fluid velocity at the boundary:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: bottom;margin:auto;width: 100%;"
|-
| <math>{\mathit{\boldsymbol{v}}}_{\phi }\cdot {\mathit{\boldsymbol{n}}}_{p}\, =-{\mathit{\boldsymbol{v}}}_{p}\cdot {\mathit{\boldsymbol{n}}}_{p}-</math><math>{\mathit{\boldsymbol{v}}}_{\psi }\cdot {\mathit{\boldsymbol{n}}}_{p}</math> <math display="inline">on\, P\in {\Gamma }_{B}</math>,
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(22)
|}


where <math display="inline">{\mathit{\boldsymbol{v}}}_{p}</math> is the boundary velocity due to the structural displacement at point ''P''.''' '''The boundary term <math display="inline">{\boldsymbol{b}}_{{\Gamma }_{B}}</math> can be expresses in matrix form as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{b}}_{{\Gamma }_{B}}\right] }^{n+1}=\overline{\overline{\boldsymbol{E}}}\mathit{\boldsymbol{\, }}{\left[ {\boldsymbol{v}}_{{\Gamma }_{B}}\right] }^{n+1}</math>
|}
|  style="text-align: right;width: 5px;text-align: right;white-space: nowrap;"|(23)
|}


Where <math display="inline">\left[ {\boldsymbol{v}}_{{\Gamma }_{B}}\right]</math> ''' '''is the vector containing the values of <math display="inline">{\mathit{\boldsymbol{v}}}_{p}</math> for those points <math display="inline">p\in {\Gamma }_{B}</math>, and <math display="inline">\overline{\overline{\boldsymbol{E}}}</math> is the assembled boundary condition matrix. The coupling term that relates the boundary velocity with the structural displacement can be expressed in matrix form as:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{v}}_{{S,\Gamma }_{B}}\right] }^{n+1}=</math><math>\frac{2}{\Delta t}{\left[ {\mathit{\boldsymbol{\Delta }}\boldsymbol{u}}_{{\Gamma }_{B}}\right] }^{n+1}-</math><math>{\left[ {\boldsymbol{v}}_{{S,\Gamma }_{B}}\right] }^{n}</math>
|}
|  style="text-align: right;width: 5px;text-align: right;white-space: nowrap;"|(24)
|}


Using the interpolation matrix we obtain:

{| class="formulaSCP" style="width: 100%;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{v}}_{{F,\Gamma }_{B}}\right] }^{n+1}=\beta {\overline{\overline{\mathit{\boldsymbol{I}}}}}^{S\rightarrow F}\, {\left[ {\mathit{\boldsymbol{\Delta }}\boldsymbol{u}}_{{\Gamma }_{B}}\right] }^{n+1}+</math><math>{\left[ {\boldsymbol{v}}_{{F,\Gamma }_{B}}\right] }^{n}</math>
|}
|  style="width: 5px;text-align: right;white-space: nowrap;"|(25)
|}


where <math display="inline">\beta =2/\Delta t</math>. Assembling the equations above, the resulting global system of equations is:

{| class="formulaSCP" style="width: 100%;border-collapse: collapse;width: 100%;text-align: center;" 
|-
| 
{| style="vertical-align: top;margin:auto;width: 100%;"
|-
|

{| class="formulaSCP" style="width: 86%;border-collapse: collapse;width: 100%;text-align: center;" 
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{S}}}}_{II}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{S}}}}_{I{\Gamma }_{B}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| 
|}
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\Delta \boldsymbol{u}}_{I}</math>
|}
|  style="border-left: 1pt solid black;text-align: right;white-space: nowrap;"|n+1
|  rowspan='6' style="text-align: center;white-space: nowrap;"|=
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| 
|}
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{a}}_{I}</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|n+1
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}I}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{S}}}}_{{\Gamma }_{B}{\Gamma }_{B}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>-\overline{\overline{\mathit{\boldsymbol{C}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
|  style="border-left: 1pt solid black;border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\Delta \boldsymbol{u}}_{{\Gamma }_{B}}</math>
|}
|  style="border-left: 1pt solid black;text-align: right;white-space: nowrap;"|
|  style="border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{a}}_{{\Gamma }_{B}}^{\ast }</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\boldsymbol{I}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>-\alpha {\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
|  style="border-left: 1pt solid black;border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{P}}_{{S,\Gamma }_{B}}^{\phi }</math>
|}
|  style="border-left: 1pt solid black;text-align: right;white-space: nowrap;"|
|  style="border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\mathit{\boldsymbol{I}}}}}^{F\rightarrow S}\boldsymbol{d}</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{L}}}}_{II}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{L}}}}_{I{\Gamma }_{B}}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
|  style="border-left: 1pt solid black;border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{\phi }}_{I}</math>
|}
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| 
|}
|  style="border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{b}}_{I}</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math display="inline">\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{L}}}}_{{\Gamma }_{B}I}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>{\overline{\overline{\boldsymbol{L}}}}_{{\Gamma }_{B}{\Gamma }_{B}}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>-\overline{\overline{\mathit{\boldsymbol{E}}}}</math>
|}
|  style="border-left: 1pt solid black;border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{\phi }}_{{\Gamma }_{B}}</math>
|}
|  style="border-left: 1pt solid black;text-align: right;white-space: nowrap;"|
|  style="border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\boldsymbol{0}</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|
|-
| 
{| style="border-left: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>-\beta {\overline{\overline{\mathit{\boldsymbol{I}}}}}^{S\rightarrow F}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\mathit{\boldsymbol{0}}}}</math>
|}
| 
{| style="border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>\overline{\overline{\boldsymbol{I}}}</math>
|}
|  style="border-left: 1pt solid black;border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\boldsymbol{v}}_{{F,\Gamma }_{B}}</math>
|}
|  style="border-left: 1pt solid black;text-align: right;white-space: nowrap;"|
|  style="border-right: 1pt solid black;text-align: right;white-space: nowrap;"|
| 
{| style="border-left: 1pt solid black;border-right: 1pt solid black;margin:auto;width: 100%;"
|-
| <math>{\left[ {\boldsymbol{v}}_{{F,\Gamma }_{B}}\right] }^{n}</math>
|}
|  style="border-left: 1pt solid black;vertical-align: top;text-align: right;white-space: nowrap;"|
|}



| <span id='_Ref35585258'></span>(26)
|}


The monolithic coupling has the advantage of avoiding the iterative procedure required by the partitioned coupling, preventing iterative convergence issues. Instead, it requires to solve the system of equations given in Eq. <span id='cite-_Ref35585258'></span>[[#_Ref35585258|(26)]] . Due to the very different field variables involved, this is an ill-conditioned system, requiring the use of a robust direct solver. In this work, we have used the shared-memory multiprocessing parallel direct sparse solver Intel-MKL’s PARDISO [<span id='cite-34'></span>[[#34|34]]].

==5. Application examples==

===5.1 Flexible catamaran in oblique waves===

In this example, a flexible catamaran will be analyzed advancing in an oblique monochromatic wave. The catamaran consists of two Wigley hulls connected by flexible beams. <span id='cite-_Ref54606255'></span>[[#_Ref54606255|Figure 3]] shows the structural components as well as their layout and dimensions. Wave particulars are chosen to match the first torsional dry modal frequency. The main particulars of the ship, wave environment, and structural details are provided in <span id='cite-_Ref54607474'></span>[[#_Ref54607474|Table 1]].

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image3.jpg|600px]] </div>

<div id="_Ref54606255" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 3: Wigley catamaran main dimensions</div>

<div id="_Ref54607474" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 1: Main particulars of the Wigley Catamaran</div>

{| style="width: 69%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Waterline length'''
|  style="border: 1pt solid black;text-align: right;"|50 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Distance between hulls'''
|  style="border: 1pt solid black;text-align: right;"|25 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Draft'''
|  style="border: 1pt solid black;text-align: right;"|3.125 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Wigley hull Breadth'''
|  style="border: 1pt solid black;text-align: right;"|5 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Wigley hull Amidships section coefficient, Cm'''
|  style="border: 1pt solid black;text-align: right;"|0.6667
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Displacement [kg]'''
|  style="border: 1pt solid black;text-align: right;"|698000 kg
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Steel density'''
|  style="border: 1pt solid black;text-align: right;"|7844.67 kg/m<sup>3</sup>
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Steel Young modulus'''
|  style="border: 1pt solid black;text-align: right;"|210 GPa
|-
|  rowspan='4' style="border: 1pt solid black;text-align: center;"|'''Steel plates thickness'''
|  style="border: 1pt solid black;text-align: center;"|'''Hulls'''
|  style="border: 1pt solid black;text-align: right;"|0.04205 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Decks'''
|  style="border: 1pt solid black;text-align: right;"|0.04205 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Bulkheads'''
|  style="border: 1pt solid black;text-align: right;"|0.04205 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Connecting Beams'''
|  style="border: 1pt solid black;text-align: right;"|0.055 m
|-
|  rowspan='3' style="border: 1pt solid black;text-align: center;"|'''Center of gravity'''
|  style="border: 1pt solid black;text-align: center;"|'''XG'''
|  style="border: 1pt solid black;text-align: right;"|0 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''YG'''
|  style="border: 1pt solid black;text-align: right;"|0 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''ZG'''
|  style="border: 1pt solid black;text-align: right;"|0.2195 m
|-
|  rowspan='3' style="border: 1pt solid black;text-align: center;"|'''Radii of gyration'''
|  style="border: 1pt solid black;text-align: center;"|'''rxx'''
|  style="border: 1pt solid black;text-align: right;"|12.45 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''ryy'''
|  style="border: 1pt solid black;text-align: right;"|13.07 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''rzz'''
|  style="border: 1pt solid black;text-align: right;"|17.88 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Froude number'''
|  style="border: 1pt solid black;text-align: right;"|0.215
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Advancing velocity'''
|  style="border: 1pt solid black;text-align: right;"|4.755 m/s
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Wave incident angle'''
|  style="border: 1pt solid black;text-align: right;"|63.45 º
|-
|  rowspan='4' colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Incident wave amplitudes'''
|  style="border: 1pt solid black;text-align: right;"|0 m 
|-
|  style="border: 1pt solid black;text-align: right;"|0.01m
|-
|  style="border: 1pt solid black;text-align: right;"|0.1 m
|-
|  style="border: 1pt solid black;text-align: right;"|0.5 m
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Incident wave period'''
|  style="border: 1pt solid black;text-align: right;"|5.36 s
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Incident wave encountering period '''
|  style="border: 1pt solid black;text-align: right;"|4.27 s
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Incident wave encountering frequency '''
|  style="border: 1pt solid black;text-align: right;"|0.2342 Hz
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Water depth'''
|  style="border: 1pt solid black;text-align: right;"|25 m
|}


In this case study, a hydro-elastic analysis will be carried out using both, loose (one-way) and tight (two-ways) coupling formulations. For each formulation linear and non-linear geometry models for the structural analysis will be considered.

In order to carry out the loose coupling, first the seakeeping hydrodynamics simulation is carried out assuming the ship as a rigid body (uncoupled from the structural problem). Then, the dynamic pressure obtained will be used as a pressure load in the posteriori loosely coupled structural simulation.

The global frame of reference is located at the center of the ship and on the mean water level. The ship is supposed to advance forward in the negative OX direction. But since the global frame of reference moves forward with the ship, the forward speed is modeled as a water current in the positive OX direction. For the rigid-body approximation, the center of gravity will be restricted to move in surge and sway, and rotate in yaw to avoid any drifting (modelling the effect of the propulsion and steering systems).  In the structural simulations, the points B1 and S2 (see <span id='cite-_Ref54947500'></span>[[#_Ref54947500|Figure 4]]) will be restricted to move in the forward OX direction, while points B2 and S1 will be restricted to move in the transversal OY direction. These restrictions are coherent with those used for the rigid body approximation.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
<big> [[Image:Draft_Garcia-Espinosa_378827043-image4.jpg|522px]] </big></div>

<div id="_Ref54947500" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 4: Data collection points.</div>

First of all, a structural modal analysis is carried out in dry. <span id='cite-_Ref54854175'></span>[[#_Ref54854175|Figure 5]] shows the main global structural modes with lower frequencies. It is observed that the first torsional mode happens at 0.2342 Hz. The incident wave length and direction, and the advancing velocity are adjusted to force this wave encountering frequency and to induce the torsional response. <span id='cite-_Ref54856387'></span>[[#_Ref54856387|Figure 6]] shows that the wave is selected to induce the torsion by a phase delay between the hulls pitch rotation. Then selecting an advancing velocity of 4.755 m/s the target wave encountering frequency is obtained.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image5.jpeg|432px]] </div>

<div id="_Ref54854175" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 5: Structural modal analysis of the Wigley catamaran. Color fill represents dimensionless displacements.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image6.jpg|468px]] </div>

<div id="_Ref54856387" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 6: Incident wave length and direction setup.</div>

Computational domain

The computational domain consists of the near field and far field. The near field is an elliptical cylinder around the ship where mesh refinement is applied to solve accurately the wave diffraction-radiation problem. The far field goes from the near field to the edge of a circular cylinder of 300 meters in diameter. In this far field, diffracted and radiated waves are dissipated. <span id='cite-_Ref54868330'></span>[[#_Ref54868330|Figure 7]] shows the computational domain and mesh used. <span id='cite-_Ref54869289'></span>[[#_Ref54869289|Table 2]] reports the mesh sizes used in the near field free surface and the structural elements.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
<big> [[Image:Draft_Garcia-Espinosa_378827043-image7.jpeg|600px]] </big></div>

<div id="_Ref54868330" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 7: Computational domain and mesh.</div>

<div id="_Ref54869289" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 2: Near field mesh sizes</div>

{| style="width: 72%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Problem'''
|  style="border: 1pt solid black;text-align: center;"|'''Surface'''
|  style="border: 1pt solid black;text-align: center;"|'''Mesh type'''
|  style="border: 1pt solid black;text-align: center;"|'''Mesh size'''
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Seakeeping'''
|  style="border: 1pt solid black;text-align: center;"|Free Surface
|  style="border: 1pt solid black;text-align: center;"|Unstructured
|  style="border: 1pt solid black;text-align: center;"|1m
|-
|  style="border: 1pt solid black;text-align: center;"|Wet Hulls
|  style="border: 1pt solid black;text-align: center;"|Unstructured
|  style="border: 1pt solid black;text-align: center;"|1m
|-
|  rowspan='4' style="border: 1pt solid black;text-align: center;"|'''Structural'''
|  style="border: 1pt solid black;text-align: center;"|Hulls
|  style="border: 1pt solid black;text-align: center;"|Unstructured
|  style="border: 1pt solid black;text-align: center;"|1m
|-
|  style="border: 1pt solid black;text-align: center;"|Bulkheads
|  style="border: 1pt solid black;text-align: center;"|Unstructured
|  style="border: 1pt solid black;text-align: center;"|1m
|-
|  style="border: 1pt solid black;text-align: center;"|Decks
|  style="border: 1pt solid black;text-align: center;"|Unstructured
|  style="border: 1pt solid black;text-align: center;"|1m
|-
|  style="border: 1pt solid black;text-align: center;"|Beams
|  style="border: 1pt solid black;text-align: center;"|Structured symmetric
|  style="border: 1pt solid black;text-align: center;"|0.5mx0.166m
|}


<div id="_Ref55467424" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 3: Numerical simulation particulars</div>

{| style="width: 61%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  rowspan='3' style="border: 1pt solid black;text-align: center;"|'''Structural'''

'''problem'''
|  style="border: 1pt solid black;text-align: center;"|'''Number of nodes '''
|  style="border: 1pt solid black;text-align: center;"|14306
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of degrees of freedom'''
|  style="border: 1pt solid black;text-align: center;"|85836
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of triangles'''
|  style="border: 1pt solid black;text-align: center;"|28418
|-
|  rowspan='3' style="border: 1pt solid black;text-align: center;"|'''Seakeeping'''

'''problem'''
|  style="border: 1pt solid black;text-align: center;"|'''Number of nodes'''
|  style="border: 1pt solid black;text-align: center;"|43775 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of degrees of freedom'''
|  style="border: 1pt solid black;text-align: center;"|43775
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of tetrahedrons'''
|  style="border: 1pt solid black;text-align: center;"|215056
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Time step'''
|  style="border: 1pt solid black;text-align: center;"|0.05s
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Number of time steps'''
|  style="border: 1pt solid black;text-align: center;"|1000
|}


Dynamic analysis

In order to compare the dynamics of the ship considered as a rigid body or as an elastic structure, a number of dynamic parameters are defined based on the vertical displacement of five points. <span id='cite-_Ref54947500'></span>[[#_Ref54947500|Figure 4]] shows the location of those points, and <span id='cite-_Ref54947486'></span>[[#_Ref54947486|Table 4]] provides the definition of the dynamic parameters to be compared.

<div id="_Ref54947486" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 4: Description of dynamic parameters</div>

{| style="width: 77%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Heave [m]'''
|  style="border: 1pt solid black;text-align: center;"|<math>\mathit{\boldsymbol{Z}}</math>
|  style="border: 1pt solid black;text-align: center;"|<math>\frac{{\Delta z}_{b1}+{\Delta z}_{s1}+{\Delta z}_{b2}+{\Delta z}_{s2}}{4}</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Pitch hull 1 [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math>{\mathit{\boldsymbol{\theta }}}_{\mathit{\boldsymbol{1}}}</math>
|  style="border: 1pt solid black;text-align: center;"|<math>\frac{{\Delta z}_{b1}-{\Delta z}_{s1}}{30}</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Pitch hull 2 [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math>{\mathit{\boldsymbol{\theta }}}_{\mathit{\boldsymbol{2}}}</math>
|  style="border: 1pt solid black;text-align: center;"|<math>\frac{{\Delta z}_{b2}-{\Delta z}_{s2}}{30}</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Pitch ship [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math>\mathit{\boldsymbol{\theta }}</math>
|  style="border: 1pt solid black;text-align: center;"|<math>0.5({\theta }_{1}+{\theta }_{2})</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Roll ship [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math>\mathit{\boldsymbol{\phi }}</math>
|  style="border: 1pt solid black;text-align: center;"|<math>\frac{0.5\left( {\Delta z}_{b2}+{\Delta z}_{s2}\right) -0.5\left( {\Delta z}_{b1}+{\Delta z}_{s1}\right) }{25}</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Torsion [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math>\boldsymbol{\Tau }</math>
|  style="border: 1pt solid black;text-align: center;"|<math>{\theta }_{1}-{\theta }_{2}</math>
|-
|  style="border: 1pt solid black;text-align: center;"|'''Transverse deflection [%]'''
|  style="border: 1pt solid black;text-align: center;"|<math>\boldsymbol{\Gamma }</math>
|  style="border: 1pt solid black;text-align: center;"|<math>\frac{Z-{\Delta z}_{C}}{25}\, 100</math>
|}


Dynamic analysis in the absence of incident waves

First the dynamic response of the ship in the absence of incident waves and with forward speed is analyzed. In this case, the ship is subject to the following structural loads: self weight, hydrostatic pressure, and dynamic pressure induced by the forward speed.  <span id='cite-_Ref64879482'></span>[[#_Ref64879482|Table 5]] provides the results for different numerical approaches for the dynamic parameters.

<div id="_Ref64879482" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 5: Equilibrium values with forward speed and in the absence of incident waves </div>

{| style="width: 100%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Coupling formulation'''
|  style="border: 1pt solid black;text-align: center;"|'''Structural model'''
|  style="border: 1pt solid black;text-align: center;"|<math display="inline">{\boldsymbol{Z}}_{\boldsymbol{0}}</math>''' [m]'''
|  style="border: 1pt solid black;text-align: center;"|<math display="inline">{\boldsymbol{\theta }}_{\boldsymbol{0}}</math>''' [m]'''
|  style="border: 1pt solid black;text-align: center;"|<math display="inline">{\boldsymbol{\phi }}_{\boldsymbol{0}}</math>''' [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math display="inline">{\boldsymbol{T}}_{\boldsymbol{0}}</math>''' [rad]'''
|  style="border: 1pt solid black;text-align: center;"|<math display="inline">{\boldsymbol{\Gamma }}_{\boldsymbol{0}}</math>''' [%]'''
|-
|  style="border: 1pt solid black;text-align: center;"|Uncoupled
|  style="border: 1pt solid black;text-align: center;"|Rigid Body
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|
|  style="border: 1pt solid black;text-align: center;"|
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Loose
|  style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-0.047
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;"|1.271
|-
|  style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-0.047
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;"|1.028
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Tight
|  style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-0.047
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;"|1.271
|-
|  style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-0.047
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|<math display="inline">\boldsymbol{\approx }</math>0
|  style="border: 1pt solid black;text-align: center;"|1.028
|}


As expected, <math display="inline">{Z}_{0}</math> and <math display="inline">{\Gamma }_{0}</math> are non-negligible values. It is known that the dynamic pressure of a ship advancing with forward speed induce a sinkage of the ship, which in this case is represented by <math display="inline">{Z}_{0}</math>. Moreover, at equilibrium, the hydrodynamic pressure and self-weight loads induce a transversal deflection represented by <math display="inline">{\Gamma }_{0}</math>.

It is observed that this equilibrium deflection <math display="inline">{\Gamma }_{0}</math> does not depend on the coupling strategy (tight or loose), since in equilibrium there are not hydrodynamic radiation loads. But it depends on the geometric model (linear or non-linear), showing a larger deflection for the linear one. This confirms the necessity of using a non-linear geometry model for sufficiently elastic structures like this catamaran.

If incident wave loads are considered, the larger the wave amplitudes, the larger the differences between the linear and non-linear geometry model will become. This is shown later in the dynamic analysis for different wave amplitudes.

Dynamic analysis with incident wave amplitude: A<sub>w</sub> =0.5m

In this section, a dynamic analysis is carried including the incident wave load of a wave with 0.5 meter in amplitude. <span id='cite-_Ref55291295'></span>[[#_Ref55291295|Figure 8]] compares the dynamic parameters across the different numerical approaches, and <span id='cite-_Ref55561983'></span>[[#_Ref55561983|Figure 9]] compare the Von Misses stress at point C. Similar values are obtained by the monolithic and partitioned strategies, so only one is showed as tight coupling. The following conclusions are obtained:

:1. Heave and Pitch motions: the loose coupling strategies provide very close results to the rigid body, while the tight coupling significantly differs. Moreover, in the tight coupling, significant differences are observed between the geometric linear and non-linear structural models.

:2. Roll motion: all coupled strategies provide very similar results to the rigid body.

:3. Torsional displacements: Significant differences are observed between the loose and tight strategies. However, no significant differences between using the geometric linear or non-linear structural models.

:4. Transverse deflection: Significant differences are observed across the four coupling strategies.

:5. There are large differences in the comparison of Von Misses stress measured at point C, located at the flexible beam structure.

In this case study, it is observed that the elastic behavior of the beams connecting the twin hulls has a significant impact on the hydroelasticity of the ship. This impact makes the results obtained from the loose formulation to differ from those obtained with the tight formulation. Even though the heave, roll and pitch movements are small, the geometric non-linear structural behavior of the beams are also relevant for the global hydroelastic behavior of the ship. <span id='cite-_Ref55539586'></span>[[#_Ref55539586|Figure 10]] shows the differences of the instantaneous structural displacements at time=45s, and <span id='cite-_Ref55539602'></span>[[#_Ref55539602|Figure 11]] shows snapshots of the free surface elevation for the tight-nonlinear approach.

Looking at <span id='cite-_Ref55291295'></span>[[#_Ref55291295|Figure 8]], it is observed that the ship movements are small and therefore the use of a linear model is correct for the seakeeping hydrodynamics. On the other hand, a geometric non-linear corotational formulation has been chosen for the structural model, and there is a reason for that. Rigid body movements of a ship are expected to be dominant compared to structural displacements. And linear structural models are not capable of reproducing rigid body movements without inducing spurious structural strains (and stresses). These spurious stresses can be larger than the structural ones if the rigid body movements are large enough. On the other hand the corotational formulation is capable of reproducing non-small rigid-body movements without inducing spurious structural strains (and stresses).

Dynamic analysis for different incident wave amplitudes

The effect of the incident wave amplitude is also analyzed in this section. <span id='cite-_Ref65055494'></span>[[#_Ref65055494|Figure 12]], <span id='cite-_Ref84397301'></span>[[#_Ref84397301|Figure 13]], and <span id='cite-_Ref84397302'></span>[[#_Ref84397302|Figure 14]] compare the dynamic parameters <math display="inline">Z</math>, <math display="inline">\theta</math> , and <math display="inline">\Gamma</math>  for three wave amplitudes: Aw=0.01m; Aw=0.1m; and Aw=0.5m. It is observed that, as the wave amplitude decreases, the differences between the different numerical approximations also decreases. For instance, m the differences in <math display="inline">\Gamma</math>  for Aw=0.5 are in the order of 2.5%, while for Aw=0.01m the differences are in the order of 0.2%. Actually the dynamic parameters for Aw=0.01m are very similar to those reported in <span id='cite-_Ref64879482'></span>[[#_Ref64879482|Table 5]] (equilibrium parameters in the absence of incident waves), where the transverse deflection in equilibrium are different for the geometric linear and non-linear models.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
<big> [[Image:Draft_Garcia-Espinosa_378827043-image8.jpeg|600px]] </big></div>

<div id="_Ref55291295" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 8: Comparison of dynamic parameters for  A<sub>w</sub>=0.5m.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image9.jpeg|384px]] </div>

<div id="_Ref55561983" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 9: Comparison of Von Misses stresses at point C (0,0,2.25) for A<sub>w</sub>=0.5m.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image10.jpeg|600px]] </div>

<div id="_Ref55539586" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 10: Structural displacements snapshot at time=45s. Colorfill represents total displacements.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image11.jpeg|600px]] </div>

<div id="_Ref55539602" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 11: Free surface elevation snapshots computed by the monolithic-nonlinear approach.</div>

<span id='cite-_Ref75959740'></span>[[#_Ref75959740|Figure 15]] shows snapshots of the catamaran at the same time step for the monolithic coupling. Differences between the geometric linear and non-linear models are easily observed. It is difficult to understand why the geometric linear model provides larger transverse deflections due to the complexity of the problem, where bending and torsion are happening simultaneously. Hence the importance of developing numerical tools capable of simulating the hydro-structural dynamics.

Computational performance

In the partitioned coupling, the PARDISO direct solver is used for both, the hydrodynamics and structural parts. The fluid system of equations remains unchanged, requiring the solver to compute the approximate inversion of the structural system only once in the case of the tight-linear approach. However, the structural system has to be updated when using the geometric non-linearity, requiring to compute the approximate inversion of the structural system at every iteration. It is required only once for the linear approximation.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image12.jpg|486px]] </div>

<span id='_Ref65055494'></span><div id="_Ref71711618" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 12: Comparison of vertical displacement <math display="inline">Z</math>[m] for three incident wave amplitudes.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image13.jpg|486px]] </div>

<span id='_Ref84397301'></span><div id="_Ref71711619" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 13: Comparison of average pitch <math display="inline">\theta</math> [rad] for three incident wave amplitudes.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image14.jpg|486px]] </div>

<div id="_Ref84397302" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 14: Comparison of transverse deflection <math display="inline">\Gamma</math> [%] for three incident wave amplitudes.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image15.jpeg|438px]] </div>

<div id="_Ref75959740" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 15: Snapshots at time=43s for incident wave amplitude A=0.5m. Structural deformation is scaled by a factor of 2. </div>

In the partitioned strategy, convergence is achieved when the maximum relative tolerance of the structural displacements is below 0.001. This tolerance value has been obtained from experience by ensuring that the monolithic and partitioned formulations provide similar results. A larger tolerance value will result in loss of convergence within the time steps and divergence of the solution over time.

In the monolithic coupling, the PARDISO direct solver is also used for the global system, requiring to compute the approximate inversion at every iteration for the non-linear geometry case, but only once for the linear.

This case study was run on a computer server with twenty four real CPU cores. Two OpenMP threads are used to run the seakeeping and structural problems, using twelve cores each of them. In the monolithic coupling, the global coupled system is assembled and solved within the seakeeping thread using the twenty four cores. <span id='cite-_Ref55467407'></span>[[#_Ref55467407|Table 6]]  reports the CPU times for each approach.

Looking at <span id='cite-_Ref55467407'></span>[[#_Ref55467407|Table 6]] it is observed that the loose formulation is about 4 times faster than the tight formulation with the monolithic strategy, the use of the linear model is about ten times faster than the non-linear geometry, and the monolithic strategy is about four times faster than the partitioned one. It has to be taken into account that the number of structural degrees of freedom is about double the number of the hydrodynamic ones (see <span id='cite-_Ref55467424'></span>[[#_Ref55467424|Table 3]]).

<div id="_Ref55467407" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 6: CPU time report for incident wave amplitude A=0.5m.</div>

{| style="width: 100%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Coupling formulation'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Structural model'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Solver strategy'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Computational time (min)'''
|  colspan='2'  style="border: 1pt solid black;text-align: center;vertical-align: top;"|'''Iterations/step'''
|-
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|'''Coupling'''
|  style="border: 1pt solid black;text-align: center;"|'''Structural'''
|-
|  style="border: 1pt solid black;text-align: center;"|Uncoupled
|  style="border: 1pt solid black;text-align: center;"|Rigid Body
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|4
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-
|  style="border: 1pt solid black;text-align: center;"|-
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Loose
|  style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;"|1-way
|  style="border: 1pt solid black;text-align: center;"|10.2
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;"|1-way
|  style="border: 1pt solid black;text-align: center;"|95.2
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-
|  style="border: 1pt solid black;text-align: center;"|3
|-
|  rowspan='4' style="border: 1pt solid black;text-align: center;"|Tight
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;"|Partitioned
|  style="border: 1pt solid black;text-align: center;"|175.2
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|7
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  style="border: 1pt solid black;text-align: center;"|Monolithic
|  style="border: 1pt solid black;text-align: center;"|42,1
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;"|Partitioned
|  style="border: 1pt solid black;text-align: center;"|1800
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|8
|  style="border: 1pt solid black;text-align: center;"|7
|-
|  style="border: 1pt solid black;text-align: center;"|Monolithic
|  style="border: 1pt solid black;text-align: center;"|420
|  style="border: 1pt solid black;text-align: center;vertical-align: top;"|-
|  style="border: 1pt solid black;text-align: center;"|9
|}


===5.2 Analysis of a large floating structure (LFS)===

In this section the loose and tight coupling strategies will be compared when analyzing the elastic response of a LFS under an incident monochromatic wave. <span id='cite-_Ref55204710'></span>[[#_Ref55204710|Figure 16]] shows the main dimensions of the LFS as well as the spacing between longitudinal and transversal bulkheads, the dimensions of the computational domain, and the computational FEM mesh. The global system of reference is located at the geometric center point of the LFS, with the OX axis along the longitudinal direction, the OZ axis along the upwards vertical direction, and the mean water level at z=0.

The LFS is a reticulated structure made of fiber reinforced plastic (FRP). The points of the lines located at forward end (x=-100, z=0) and backward end (x=100, z=0) are restricted to move and rotate except for rotations around the OY axis (hinge constraints).

<span id='cite-_Ref54607474'></span>[[#_Ref54607474|Table 1]] provides the main particulars of the LFS and the incident wave, and <span id='cite-_Ref55297829'></span>[[#_Ref55297829|Table 8]] provides the details about the computational FEM mesh. The wave period is chosen to approximate the wave length to the length of the LFS in order to induce large bending moments. The vertical displacements will be collected at the following three points: L(-50,0,2.5), C(0,0,2.5) and R(50,0,2.5).

In this academic case study, the rigid body approximation implies that the LFS does not move due to the restrictions at the forward and backward ends. Then the dynamic pressure obtained will have no radiation component (only Froude-Krylov and diffraction). On the other hand, tight coupling approximation will take into account the radiation component due to the elastic displacements. In order to evaluate how significant the radiation is compared to the Froude-Krylov and diffraction components, the vertical displacement of three points will be compared. These displacements will be computed using the loose and tight coupling strategies.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 7: LFS and wave particulars</div>

{| style="width: 43%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Length'''
|  style="border: 1pt solid black;text-align: right;"|200 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Breadth'''
|  style="border: 1pt solid black;text-align: right;"|40 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Draft'''
|  style="border: 1pt solid black;text-align: right;"|2.5 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''LFS height'''
|  style="border: 1pt solid black;text-align: right;"|5m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Displacement [kg]'''
|  style="border: 1pt solid black;text-align: right;"|20500000 kg
|-
|  style="border: 1pt solid black;text-align: center;"|'''FRP structural weight'''
|  style="border: 1pt solid black;text-align: right;"|20500000 kg
|-
|  style="border: 1pt solid black;text-align: center;"|'''FRP density'''
|  style="border: 1pt solid black;text-align: right;"|2000 kg/m<sup>3</sup>
|-
|  style="border: 1pt solid black;text-align: center;"|'''FRP Young modulus'''
|  style="border: 1pt solid black;text-align: right;"|21 GPa
|-
|  style="border: 1pt solid black;text-align: center;"|'''FRP plates thickness'''
|  style="border: 1pt solid black;text-align: right;"|0.249 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Wave incident angle'''
|  style="border: 1pt solid black;text-align: right;"|0 º
|-
|  style="border: 1pt solid black;text-align: center;"|'''Wave period'''
|  style="border: 1pt solid black;text-align: right;"|14 s
|-
|  style="border: 1pt solid black;text-align: center;"|'''Wave amplitude'''
|  style="border: 1pt solid black;text-align: right;"|0.5 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Wave length '''
|  style="border: 1pt solid black;text-align: right;"|200.4 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Water depth'''
|  style="border: 1pt solid black;text-align: right;"|25 m
|}


<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image16.jpeg|600px]] </div>

<div id="_Ref55204710" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 16: Top: LFS dimensions. Bottom left: Computational domain. Bottom right: computational mesh.</div>

<div id="_Ref55297829" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 8: Numerical simulation particulars</div>

{| style="width: 78%;margin: 1em auto 0.1em auto;border-collapse: collapse;" 
|-
|  rowspan='4' style="border: 1pt solid black;text-align: center;"|'''Structural'''

'''problem'''
|  style="border: 1pt solid black;text-align: center;"|'''Structural mesh size (triangle)'''
|  style="border: 1pt solid black;text-align: right;"|5 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of nodes'''
|  style="border: 1pt solid black;text-align: right;"|1107 
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of degrees of freedom'''
|  style="border: 1pt solid black;text-align: right;"|6642
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of triangular elements'''
|  style="border: 1pt solid black;text-align: right;"|4672
|-
|  rowspan='5' style="border: 1pt solid black;text-align: center;"|'''Seakeeping'''

'''problem'''
|  style="border: 1pt solid black;text-align: center;"|'''Free surface nearfield mesh size (triangle)'''
|  style="border: 1pt solid black;text-align: right;"|5 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Fluid domain nearfield mesh size (tetrahedron)'''
|  style="border: 1pt solid black;text-align: right;"|5 m
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of nodes'''
|  style="border: 1pt solid black;text-align: right;"|44104
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of degrees of freedom'''
|  style="border: 1pt solid black;text-align: right;"|44104
|-
|  style="border: 1pt solid black;text-align: center;"|'''Number of  tetrahedral elements'''
|  style="border: 1pt solid black;text-align: right;"|216151
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Time step'''
|  style="border: 1pt solid black;text-align: right;"|0.05 s
|-
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Number of time steps'''
|  style="border: 1pt solid black;text-align: right;"|6000
|}


<span id='cite-_Ref55376161'></span>[[#_Ref55376161|Figure 17]] compares the vertical displacements at the L, C and R points for the four coupling strategies. <span id='cite-_Ref55556586'></span>[[#_Ref55556586|Figure 18]] compares the time history of the Von Misses stresses at point C, and <span id='cite-_Ref55556619'></span>[[#_Ref55556619|Figure 19]] compares snapshots of the structural displacements and stresses. Similar values are obtained by the monolithic and partitioned strategies, so only one is showed as tight coupling. We observe that the tight formulation reports significant lower displacements and stresses than the loose formulation. This confirms that the wave radiation component cannot be considered negligible respect to the Froude-Krylov and wave diffraction components. It is also observed that for this particular case, the linear and nonlinear structural approximations provide very similar results, which is expected considering the small beam deflection obtained.

This case study was run on a computer server with twenty four real CPU cores. Two OpenMP threads are used to run the seakeeping and structural problems, using twelve cores each of them. In the monolithic coupling, the global coupled system is assembled and solved within the seakeeping thread using twenty four cores. <span id='cite-_Ref55467743'></span>[[#_Ref55467743|Table 9]] reports the CPU times for each approach.

Looking at <span id='cite-_Ref55467743'></span>[[#_Ref55467743|Table 9]] it is observed that the monolithic strategy is about three times faster than the partitioned one. It has to be taken into account that the number of structural degrees of freedom is about seven times smaller than the hydrodynamic ones (see <span id='cite-_Ref55297829'></span>[[#_Ref55297829|Table 8]]), and the impact of the structural on the computational time will be lower than in the catamaran case study.

<div id="_Ref55467743" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Table 9: CPU time report</div>

{| style="width: 100%;border-collapse: collapse;" 
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Coupling formulation'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Structural model'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Coupling strategy'''
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|'''Computational time (min)'''
|  colspan='2'  style="border: 1pt solid black;text-align: center;"|'''Iterations/step'''
|-
|  style="border: 1pt solid black;text-align: center;"|'''Coupling'''
|  style="border: 1pt solid black;text-align: center;"|'''Structural'''
|-
|  style="border: 1pt solid black;text-align: center;"|'''-'''
|  style="border: 1pt solid black;text-align: center;"|Rigid Body
|  style="border: 1pt solid black;text-align: center;"|Uncoupled
|  style="border: 1pt solid black;text-align: center;"|7.8
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|-
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Loose
|  style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;"|One way
|  style="border: 1pt solid black;text-align: center;"|93
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;"|One way
|  style="border: 1pt solid black;text-align: center;"|248
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|2
|-
|  rowspan='4' style="border: 1pt solid black;text-align: center;"|Tight
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Linear
|  style="border: 1pt solid black;text-align: center;"|Partitioned
|  style="border: 1pt solid black;text-align: center;"|338
|  style="border: 1pt solid black;text-align: center;"|11
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  style="border: 1pt solid black;text-align: center;"|Monolithic
|  style="border: 1pt solid black;text-align: center;"|104
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|1
|-
|  rowspan='2' style="border: 1pt solid black;text-align: center;"|Non-Linear geometry
|  style="border: 1pt solid black;text-align: center;"|Partitioned
|  style="border: 1pt solid black;text-align: center;"|2040
|  style="border: 1pt solid black;text-align: center;"|10
|  style="border: 1pt solid black;text-align: center;"|2
|-
|  style="border: 1pt solid black;text-align: center;"|Monolithic
|  style="border: 1pt solid black;text-align: center;"|644
|  style="border: 1pt solid black;text-align: center;"|-
|  style="border: 1pt solid black;text-align: center;"|4
|}


==6. Conclusions==

In this work, a 3D tightly coupled hydroelastic model fully based on FEM has been presented. The seakeeping hydrodynamics solver can take into account the effect of forward speed using the double body linearization, and the structural solver can take into account geometric nonlinearities.

The hydroelastic problem is solved using loose and tight coupling formulations. And the latter is also solved using both, the partitioned and monolithic coupling strategies. The seakeeping and structural solvers have been developed under the same programming framework, which allows to reduce the communication overheads in the partitioned coupling, and also allows the implementation of the monolithic coupling.

Two case studies have been analyzed to test the performance of both coupling strategies. The first one analyzes the structural response of a 3D flexible catamaran under an oblique wave with forward speed. The second analyzes the 3D global structural response of a reticulated large floating structure made of fiber reinforced plastic. The monolithic strategy has been implemented successfully, showing no convergence issues when solving the monolithic global system of equations. The partitioned strategy requires to set a low enough tolerance value for the coupling scheme to ensure convergence within each time step, otherwise, the solution will diverge over time.

When analyzing the response of the catamaran, it is observed that the loose formulation do not approximate well enough the results obtained by the tight formulation in terms of displacements and stresses. And neither does the geometric linear model respect the non-linear geomtry model. With regards to the large floating platform case study, it is observed that the linear and non-linear geometry results are very similar but, again, the loose formulation does not approximate well enough the tight formulation. Besides, the loose formulation seems to overestimate the stresses on the structure. Then, the analysis of both cases requires of a tightly coupled scheme to take into account the wave radiation induced by the structural displacements.

Both case studies have been used to compare the computational times required by the different coupling approaches. For the catamaran case, the monolithic strategy is about 4- faster than the partitioned one. And 3 times faster for the large floating platform. This speed up seems to be larger as the ratio of structural degrees of freedoms to hydrodynamics degrees of freedom is larger. And although the monolithic requires to solve a much bigger system of equations, the reduction in the number of iterations lead to the overall reduction of the computational time.

==Acknowledgements==

The research leading to these results has received funding from the Spanish Ministry for Economy and Competitiveness under Grant RTI2018-094744-B-C21 (NICESHIP) and under the EU’s H2020 project FIBRESHIP (grant number 723360).

The authors are thankful to Jaume Sagués, and Ovidi Casals for the technical support provided to this research.

==Compliance with ethical standards==

On behalf of all authors, the corresponding author states that there is no conflict of interest.

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image17.jpeg|444px]] </div>

<div id="_Ref55376161" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 17: Vertical displacements at the data collection points.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image18.jpeg|444px]] </div>

<div id="_Ref55556586" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 18: Von Misses stresses at point C.</div>

<div class="center" style="width: auto; margin-left: auto; margin-right: auto;">
 [[Image:Draft_Garcia-Espinosa_378827043-image19.jpeg|600px]] </div>

<div id="_Ref55556619" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
Figure 19: Snapshots of Von Misses stresses. Structural displacements are scaled by x100.</div>

<br/>

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